CESSNA SECTION 4
MODEL T182T NAV III NORMAL PROCEDURES
GFC 700 AFCS
U.S.
STARTING ENGINE (With Battery) (Continued)
18. Oil Pressure - CHECK (verify that oil pressure increases into the
GREEN BAND range in 30 to 60 seconds)
19. AMPS (M BATT and BATT S) - CHECK (verify charge shown
(positive))
20. LOW VOLTS Annunciator - CHECK (verify annunciator is not
shown)
21. NAV Light Switch - ON as required
22. AVIONICS Switch (BUS 1 and BUS 2) - ON
STARTING ENGINE (With External Power)
1. Throttle Control - OPEN 1/4 INCH
2. Propeller Control - HIGH RPM (push full in)
3. Mixture Control - IDLE CUTOFF (pull full out)
4. STBY BATT Switch:
a. TEST - (hold for 20 seconds, verify green TEST lamp does
not go off)
b. ARM - (verify that PFD comes on)
5. Engine Indication System - CHECK PARAMETERS (verify no
red X's through ENGINE page indicators)
6. BUS E Volts - CHECK (verify 24 VOLTS minimum shown)
7. M BUS Volts - CHECK (verify 1.5 VOLTS or less shown)
8. BATT S Amps - CHECK (verify discharge shown (negative))
9. STBY BATT Annunciator - CHECK (verify annunciator is shown)
10. AVIONICS Switch (BUS 1 and BUS 2) - OFF
11. MASTER Switch (ALT and BAT) - OFF
12. Propeller Area - CLEAR (verify that all people and equipment
are at a safe distance from the propeller)
13. External Power - CONNECT (to ground power receptacle)
14. MASTER Switch (ALT and BAT) - ON
15. BEACON Light Switch - ON
16. M BUS VOLTS - CHECK (verify that approximately 28 VOLTS is
shown)
If engine is warm, omit priming procedure steps 17 thru 19
below.
17. FUEL PUMP Switch - ON
(Continued Next Page)
T182TPHBUS-00 4-13
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